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You searched for: subject:"Airplanes -- Design and construction"
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[texts]Aeroplane structure - Pippard, Alfred John Sutton, 1891-

Keywords: Airplanes -- Design and construction
Downloads: 381
[texts]Aeroplane structural design - Jones, T.H
14
Keywords: Airplanes -- Design and construction
Downloads: 1,587
[texts]How to build an aeroplane - Petit, F. Robert

Keywords: Airplanes -- Design and construction
Downloads: 1,959
[texts]Manpower planning models. IV, Synthesis of cross-sectional and longitudinal models - Grinold, Richard C.;Marshall, Kneale T.
Title from cover
Keywords: AIRPLANES--DESIGN AND CONSTRUCTION
Downloads: 29
[image]High lift flow physics PIV test - NASA/Langley Research Center
Photographed on 03/17/2003. -- Model and instrumentation setup for high lift flow physics PIV test. Photographed in the 14 X 22 Foot Subsonic Tunnel, building 1212.
Keywords: Airplanes Design and construction Photog
Downloads: 4
[image]High lift flow physics PIV measurements - NASA/Langley Research Center
Photographed on 03/18/2003. -- Laser and camera set-up for PIV measurements on the Trap Wing Model. Photographed in the 14 X 22 Foot Subsonic Tunnel, building 1212.
Keywords: Airplanes Design and construction Photog
Downloads: 4
[image]2003 MSU/NASA SAA-1-562 - NASA/Langley Research Center
Photographed on 11/14/2003. -- A 6 inch diameter model 2 meters long with a rotating section to produce a 3 dimentional boundry layer over rear facing step measurements, including hot wire, pressure taps, PIV, and microphone array (32 on centerline).
Keywords: Airplanes Design and construction Photog
Downloads: 6
[image]BWB spin/tumble test model - NASA/Langley Research Center
Blended Wing Body (BWB). -- Photographed on 09/24/1999. -- Overall views of the model. Photographed in building 1145, photographic studio.
Keywords: Airplanes Design and construction Photog
Downloads: 4
[image]High lift flow physics PIV test - NASA/Langley Research Center
Photographed on 03/17/2003. -- Model and instrumentation setup for high lift flow physics PIV test. Photographed in the 14 X 22 Foot Subsonic Tunnel, building 1212.
Keywords: Airplanes Design and construction Photog
Downloads: 2
[image]2003 MSU/NASA SAA-1-562 - NASA/Langley Research Center
Photographed on 11/14/2003. -- A 6 inch diameter model 2 meters long with a rotating section to produce a 3 dimentional boundry layer over rear facing step measurements, including hot wire, pressure taps, PIV, and microphone array (32 on centerline).
Keywords: Airplanes Design and construction Photog
Downloads: 6
[image]2003 MSU/NASA SAA-1-562 - NASA/Langley Research Center
Photographed on 11/14/2003. -- A 6 inch diameter model 2 meters long with a rotating section to produce a 3 dimentional boundry layer over rear facing step measurements, including hot wire, pressure taps, PIV, and microphone array (32 on centerline).
Keywords: Airplanes Design and construction Photog
Downloads: 3
[image]High lift flow physics PIV measurements - NASA/Langley Research Center
Photographed on 03/18/2003. -- Laser and camera set-up for PIV measurements on the Trap Wing Model. Photographed in the 14 X 22 Foot Subsonic Tunnel, building 1212.
Keywords: Airplanes Design and construction Photog
Downloads: 4
[image]2003 MSU/NASA SAA-1-562 - NASA/Langley Research Center
Photographed on 11/14/2003. -- A 6 inch diameter model 2 meters long with a rotating section to produce a 3 dimentional boundry layer over rear facing step measurements, including hot wire, pressure taps, PIV, and microphone array (32 on centerline).
Keywords: Airplanes Design and construction Photog
Downloads: 4
[image]2003 MSU/NASA SAA-1-562 - NASA/Langley Research Center
Photographed on 11/14/2003. -- A 6 inch diameter model 2 meters long with a rotating section to produce a 3 dimentional boundry layer over rear facing step measurements, including hot wire, pressure taps, PIV, and microphone array (32 on centerline).
Keywords: Airplanes Design and construction Photog
Downloads: 4
[image]Trapezoidal wing model - NASA/Langley Research Center
Photographed on 09/15/98. -- Trapezoidal wing model. Views of microphone array panel in side wall and infrared windows. View of microphone cabling and infrared systems. A shot of the aft traverser mounted off the flap. Photographed in the 14 X 22 Foot Subsonic Tunnel.
Keywords: Airplanes Design and construction Photog
Downloads: 5
[image]BWB spin/tumble test model - NASA/Langley Research Center
Blended Wing Body (BWB). -- Photographed on 09/24/1999. -- Overall views of the model. Photographed in building 1145, photographic studio.
Keywords: Airplanes Design and construction Photog
Downloads: 5
[image]High lift flow physics PIV measurements - NASA/Langley Research Center
Photographed on 03/18/2003. -- Laser and camera set-up for PIV measurements on the Trap Wing Model. Photographed in the 14 X 22 Foot Subsonic Tunnel, building 1212.
Keywords: Airplanes Design and construction Photog
Downloads: 4
[image]High lift flow physics PIV measurements - NASA/Langley Research Center
Photographed on 03/18/2003. -- Laser and camera set-up for PIV measurements on the Trap Wing Model. Photographed in the 14 X 22 Foot Subsonic Tunnel, building 1212.
Keywords: Airplanes Design and construction Photog
Downloads: 5
[image]High lift flow physics PIV test - NASA/Langley Research Center
Photographed on 03/17/2003. -- Model and instrumentation setup for high lift flow physics PIV test. Photographed in the 14 X 22 Foot Subsonic Tunnel, building 1212.
Keywords: Airplanes Design and construction Photog
Downloads: 4
[image]High lift flow physics PIV measurements - NASA/Langley Research Center
Photographed on 03/18/2003. -- Laser and camera set-up for PIV measurements on the Trap Wing Model. Photographed in the 14 X 22 Foot Subsonic Tunnel, building 1212.
Keywords: Airplanes Design and construction Photog
Downloads: 5
[image]BWB spin/tumble test model - NASA/Langley Research Center
Blended Wing Body (BWB). -- Photographed on 09/24/1999. -- Overall views of the model. Photographed in building 1145, photographic studio.
Keywords: Airplanes Design and construction Photog
Downloads: 3
[image]High lift flow physics PIV measurements - NASA/Langley Research Center
Photographed on 03/18/2003. -- Laser and camera set-up for PIV measurements on the Trap Wing Model. Photographed in the 14 X 22 Foot Subsonic Tunnel, building 1212.
Keywords: Airplanes Design and construction Photog
Downloads: 4
[image]High lift flow physics PIV measurements - NASA/Langley Research Center
Photographed on 03/18/2003. -- Laser and camera set-up for PIV measurements on the Trap Wing Model. Photographed in the 14 X 22 Foot Subsonic Tunnel, building 1212.
Keywords: Airplanes Design and construction Photog
Downloads: 5
[image]BWB spin/tumble test model - NASA/Langley Research Center
Blended Wing Body (BWB). -- Photographed on 09/24/1999. -- Overall views of the model. Photographed in building 1145, photographic studio.
Keywords: Airplanes Design and construction Photog
Downloads: 7
[image]Blended wing body model - NASA/Langley Research Center
Blended Wing Body (BWB). -- Photographed on 02/10/98. -- 4% scale blended wing body model is mounted for tests in the Langley 14 x 22 Foot Subsonic Tunnel. Model with Dan Murri.
Keywords: Airplanes Design and construction Photog
Downloads: 5
[image]High lift flow physics PIV measurements - NASA/Langley Research Center
Photographed on 03/18/2003. -- Laser and camera set-up for PIV measurements on the Trap Wing Model. Photographed in the 14 X 22 Foot Subsonic Tunnel, building 1212.
Keywords: Airplanes Design and construction Photog
Downloads: 4
[image]High lift flow physics PIV test - NASA/Langley Research Center
Photographed on 03/17/2003. -- Model and instrumentation setup for high lift flow physics PIV test. Photographed in the 14 X 22 Foot Subsonic Tunnel, building 1212.
Keywords: Airplanes Design and construction Photog
Downloads: 3
[image]High lift flow physics PIV measurements - NASA/Langley Research Center
Photographed on 03/18/2003. -- Laser and camera set-up for PIV measurements on the Trap Wing Model. Photographed in the 14 X 22 Foot Subsonic Tunnel, building 1212.
Keywords: Airplanes Design and construction Photog
Downloads: 4
[image]Blended wing body model - NASA/Langley Research Center
Blended Wing Body (BWB). -- Photographed on 02/10/98. -- 4% scale blended wing body model is mounted for tests in the Langley 14 x 22 Foot Subsonic Tunnel. Model with Dan Murri.
Keywords: Airplanes Design and construction Photog
Downloads: 3
[image]High lift flow physics PIV measurements - NASA/Langley Research Center
Photographed on 03/18/2003. -- Laser and camera set-up for PIV measurements on the Trap Wing Model. Photographed in the 14 X 22 Foot Subsonic Tunnel, building 1212.
Keywords: Airplanes Design and construction Photog
Downloads: 4
[image]2003 MSU/NASA SAA-1-562 - NASA/Langley Research Center
Photographed on 11/14/2003. -- A 6 inch diameter model 2 meters long with a rotating section to produce a 3 dimentional boundry layer over rear facing step measurements, including hot wire, pressure taps, PIV, and microphone array (32 on centerline).
Keywords: Airplanes Design and construction Photog
Downloads: 5
[image]High lift flow physics PIV measurements - NASA/Langley Research Center
Photographed on 03/18/2003. -- Laser and camera set-up for PIV measurements on the Trap Wing Model. Photographed in the 14 X 22 Foot Subsonic Tunnel, building 1212.
Keywords: Airplanes Design and construction Photog
Downloads: 7
[image]High lift flow physics PIV measurements - NASA/Langley Research Center
Photographed on 03/18/2003. -- Laser and camera set-up for PIV measurements on the Trap Wing Model. Photographed in the 14 X 22 Foot Subsonic Tunnel, building 1212.
Keywords: Airplanes Design and construction Photog
Downloads: 3
[image]Trapezoidal wing model - NASA/Langley Research Center
Photographed on 09/15/98. -- Trapezoidal wing model. Views of microphone array panel in side wall and infrared windows. View of microphone cabling and infrared systems. A shot of the aft traverser mounted off the flap. Photographed in the 14 X 22 Foot Subsonic Tunnel.
Keywords: Airplanes Design and construction Photog
Downloads: 5
[image]Trapezoidal wing model - NASA/Langley Research Center
Photographed on 09/15/98. -- Trapezoidal wing model. Views of microphone array panel in side wall and infrared windows. View of microphone cabling and infrared systems. A shot of the aft traverser mounted off the flap. Photographed in the 14 X 22 Foot Subsonic Tunnel.
Keywords: Airplanes Design and construction Photog
Downloads: 10
[image]Blended wing body model - NASA/Langley Research Center
Blended Wing Body (BWB). -- Photographed on 08/14/97. -- 4% scale blended wing body model is mounted for tests in the Langley 14 x 22 Foot Subsonic Tunnel.
Keywords: Airplanes Design and construction Photog
Downloads: 8
[image]Blended wing body model - NASA/Langley Research Center
Blended Wing Body (BWB). -- Photographed on 08/14/97. -- 4% scale blended wing body model is mounted for tests in the Langley 14 x 22 Foot Subsonic Tunnel.
Keywords: Airplanes Design and construction Photog
Downloads: 11
[image]High lift flow physics PIV test - NASA/Langley Research Center
Photographed on 03/17/2003. -- Model and instrumentation setup for high lift flow physics PIV test. Photographed in the 14 X 22 Foot Subsonic Tunnel, building 1212.
Keywords: Airplanes Design and construction Photog
Downloads: 3
[texts]The theory & practice of aeroplane design - Andrews, Sydney Thomas Giles

Keywords: Airplanes -- Design and construction; Airplanes
Downloads: 1,853
[image]BWB spin/tumble test model - NASA/Langley Research Center
Blended Wing Body (BWB). -- Photographed on 09/24/1999. -- Overall views of the model. Photographed in building 1145, photographic studio.
Keywords: Airplanes Design and construction Photog
Downloads: 3
[texts]Aeroplane design, and A simple explanation of inherent stability - Barnwell, F. S
14
Keywords: Aeronautics; Airplanes -- Design and construction
Downloads: 783
[texts]Some measurements of surface-wave decay due to underwater turbulence - Green, T. A. (Thomas Allen), 1925-;Medwin, Herman.;Paquin, James Edward.
Title from cover
Keywords: AIRPLANES--MATERIALS; AIRPLANES--DESIGN AND CONSTRUCTION
Downloads: 31
[texts]Generalized performance limits for propellers, windmills and lifting rotors with axes parallel to the undisturbed flow - Gawain, Theodore Henry.
Title from cover
Keywords: AIRPLANES--MATERIALS; AIRPLANES--DESIGN AND CONSTRUCTION
Downloads: 59
[texts]Comparison of tightness of 78° machine-countersunk rivets driven in holes prepared with 78° and 82° countersinking tools - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804978&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Design and construction; Aerodynamics--Research
Downloads: 92
[texts]Tests of a stress-carrying door in compression - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806501&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Design and construction; Aerodynamics--Research
Downloads: 70
[texts]Critical combinations of shear and transverse direct stress for an infinitely long flat plate with edges elastically restrained against rotation - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806698&ix=nu&I=0&V=D&pm=1
Keywords: Airframes; Airplanes--Design and construction; Aerodynamics--Research
Downloads: 87
[texts]Determination of desirable lengths of Z- and channel-section columns for local-instability tests - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806705&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Design and construction; Aerodynamics--Research
Downloads: 86
[texts]Investigation of methods of supporting single-thickness specimens in a fixture for determination of compressive stress-strain curves - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806564&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Design and construction; Aerodynamics--Research
Downloads: 83
[texts]The Omega-value of a two-by-two matrix-differential game - Shubert, Bruno O.;Washburn, Alan R.
Title from cover
Keywords: AIRPLANES--MATERIALS; AIRPLANES--DESIGN AND CONSTRUCTION
Downloads: 35
[texts]Tests of a stress-carrying door in shear - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806509&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Design and construction; Aerodynamics--Research
Downloads: 96
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